Bristol Type 175 Britannia
For a description of the format and data included in Production Tables, see here.
Contents
Type Description
Type 175 Britannia
Initially conceived as a 42 passenger medium range "Empire" aircraft for overseas routes to Specification 2/47 to meet the requirements of OR.276 and powered by four Bristol Centaurus 663 powereplants, it was eventually produced as a low wing, 83 passenger, pressurised aircraft to Specification 2/47 Issue III. The cylindrical section of the fuselage was made up of multiple sections with a ring frame at each end, which provided the attachment to the next section. The fuselage panels were manufactured by Blackburn and General Aircraft at Dunbarton, and other parts were made hy Douglas Motors and by Bristol's own satellite at Weston-Super-Mare.The front and rear fuselage sections were connected by a much shorter central section which carried the heavier wing attachment frames. The stubs for the tail assembly were an integral part at the fuselage, with the fin and tailplane being simply bolted to these stubs. The wing tapered uniformly from centreline to tip, and was of two spar construction which, with the stiffened skin panels, formed a large torsion box occupying some 35 per cent of the wing chord. The inner and outer sections of wings were manufactured as separate parts. Fuel was stored in bag tanks within the torsion box, with four main tanks and three smaller ones. The ribs between the tanks were of sandwich construction with a corrugated inner sheet, Reduxed between the two flat outer sheets.
Control surface layout was conventional, each wing featuring wide-span double slotted flaps, in three segments, necessitated by the engine nacelles, and an outboard aileron in two segments. The flaps were electrically actuated, all remaining flight control surfaces being manually driven, with the assistance of full span servo tabs. Each aileron had five servo tabs, of which four were used to drive the surface, the fifth being connected to the rudder controls. Each elevator had four tabs, three used for flying control and one for trimming. Wing de-icing was achieved by taking heat from the engine compressors and channelling it via heat exchangers along the leading edge; the leading edge consisted of a double skin of light alloy, the inner skin being corrugated and Reduxed to the outer skin so as to provide a large number of chordwise ducts, from the extreme leading edge to ahout 14 per cent of the chord. The leading edges of the tailplane surfaces, prop assemblies, and the cockpit windshield were electrically de-iced. The steerable nose landing gear had twin wheels and retracted forward; each main gear assembly had four wheels, in a 2x2 bogey arrangement, and retracted backward into the inboard engine nacelles.
Crew consisted of pilot, copilot, navigator, and radio operator, with an auxiliary seat for a fifth cockpit crewperson -- as well as flight attendants. Avionics included radios, identification transponders, navigation and landing aids, and a nose weather radar. Passengers were accommodated in six-abreast seating with a central aisle. Cabin access was via two passenger doors, both on the port side; one was located behind the cockpit and the second behind the wing trailing edge. The cabin was equipped with up to three galleys and had toilet facilities at the front and rear. There was a row of large vertical-elliptical passenger windows on both sides of the fuselage. There were passenger doors fore and aft of the wing; for emergency exit, alternating windows could be jettisoned. There was an escape hatch on top behind the cockpit. Inflatable dinghies were stowed in the wings and in the passenger cabin for ditching at sea. For ease of maintenance, the engine cowlings were of a petal design, opening upwards and outwards. The top cowling panel could be lifted off after releasing its fasteners. The remainder of the cowling was formed by two large panels, which hinged upwards to provide access to the engine and oil cooler. The power plant units were interchangeahle for maximum flexibility. Four 2,800 e.h.p. Bristol Proteus 625 powerplants (first prototype only).
Control surface layout was conventional, each wing featuring wide-span double slotted flaps, in three segments, necessitated by the engine nacelles, and an outboard aileron in two segments. The flaps were electrically actuated, all remaining flight control surfaces being manually driven, with the assistance of full span servo tabs. Each aileron had five servo tabs, of which four were used to drive the surface, the fifth being connected to the rudder controls. Each elevator had four tabs, three used for flying control and one for trimming. Wing de-icing was achieved by taking heat from the engine compressors and channelling it via heat exchangers along the leading edge; the leading edge consisted of a double skin of light alloy, the inner skin being corrugated and Reduxed to the outer skin so as to provide a large number of chordwise ducts, from the extreme leading edge to ahout 14 per cent of the chord. The leading edges of the tailplane surfaces, prop assemblies, and the cockpit windshield were electrically de-iced. The steerable nose landing gear had twin wheels and retracted forward; each main gear assembly had four wheels, in a 2x2 bogey arrangement, and retracted backward into the inboard engine nacelles.
Crew consisted of pilot, copilot, navigator, and radio operator, with an auxiliary seat for a fifth cockpit crewperson -- as well as flight attendants. Avionics included radios, identification transponders, navigation and landing aids, and a nose weather radar. Passengers were accommodated in six-abreast seating with a central aisle. Cabin access was via two passenger doors, both on the port side; one was located behind the cockpit and the second behind the wing trailing edge. The cabin was equipped with up to three galleys and had toilet facilities at the front and rear. There was a row of large vertical-elliptical passenger windows on both sides of the fuselage. There were passenger doors fore and aft of the wing; for emergency exit, alternating windows could be jettisoned. There was an escape hatch on top behind the cockpit. Inflatable dinghies were stowed in the wings and in the passenger cabin for ditching at sea. For ease of maintenance, the engine cowlings were of a petal design, opening upwards and outwards. The top cowling panel could be lifted off after releasing its fasteners. The remainder of the cowling was formed by two large panels, which hinged upwards to provide access to the engine and oil cooler. The power plant units were interchangeahle for maximum flexibility. Four 2,800 e.h.p. Bristol Proteus 625 powerplants (first prototype only).
| Type 175 Britannia Series 310 Specification | |||||||||
| Span | Length | Height | Wing Area | Empty Wt | Max AUW | Cruise Speed | Maximum Speed | Range | Service Ceiling |
| 142 ft 3 in | 124 ft 3 in | 37 ft 6 in | 2075 sq ft | 86400 lb | 185000 lb | 357 mph/ 310 kn | 397 mph/ 345 kn | 5310 mi | 24000 ft |
| 43.36 m | 37.87 m | 11.43 m | 192.77 m2 | 39190 kg | 83915 kg | 575 km/h | 639 km/h | 8546 km | 7315 m |
- Series 100
- Initial medium range version, with 114ft fuselage length, crew of 7 and maximum passenger capacity of 90. Four 3,780 e.h.p. Bristol Proteus 705 powerplants.
- Series 250
- Mixed cargo/passenger long range version with 124ft 3in fuselage length, crew of 4-6 and maximum passenger capacity of 139. The same passenger door arrangement was retained as the Series 100, but the emergency exits were rethought, it having been recognized that the idea of popping out alternating windows was impractical. Only two windows on each side of the fuselage, above the wing, were made jettisonable, while an emergency exit door was installed in the rear of the fuselage on the left side, with two more emergency exit doors matching the rear passenger door and emergency exit door on the right. Four 4,120 e.h.p. Bristol Proteus 755 powerplants. (See Production Series - Customer Variants for individual series details)
- Series 252
- Series 250 for RAF Transport Command as Britannia C.2, fitted with heavy-duty flooring.. A large cargo door was installed in the port forward fuselage, with the passenger door integrated within it.
- Series 253
- Series 250 for RAF Transport Command as Britannia C.1, with metal flooring, capacity for 115 troops, 53 stretcher cases or equivalent cargo.
- Series 300
- Passenger-only, medium range version of Series 250.
- Series 300LR
- Original designation of Series 310.
- Series 305
- Series 300 with long range tanks but without higher gross weight.
- Series 310
- Series 300 with long-range fuel tanks, the outer wing section being built as an integral fuel tank to accommodate the extra fuel, thicker fuselage skin and strengthened landing gear for all-up weight of 175,000Ib.
- Series 320
- Series 310 to the latest modification standard. Four 4,445 e.h.p. Bristol Proteus 765 powerplants.
Britannia Civilian Customer Series Numbers
| Series | Customer |
| 101 | Prototypes with Proteus 600 series powerplants. |
| 102 | Production Series 100 for BOAC. |
| 253F | Civilianised ex-RAF Britannia C.1. |
| 301 | Prototype for 300 series. |
| 302 | Series 300 for Aeronaves de Mexico. |
| 306 | Series 305 for El Al. |
| 307 | Series 305 for Air Charter. |
| 307F | Series 307 modified as freighters. |
| 308 | Series 305 for Transcontinental SA, Argentina. |
| 308F | Series 308 modified as freighters. |
| 309 | Series 305 for Ghana Airways. |
| 311 | Prototype for 310 series. |
| 312 | Series 310 for BOAC. |
| 312F | Series 312 modified as freighters. |
| 313 | Series 310 for El Al. |
| 314 | Series 310 for Canadian Pacific Airlines. |
| 317 | Series 310 for Hunting Clan Air Transport (later BUA). |
| 318 | Series 310 for Cubana |
| 319 | Series 310 for Ghana Airways. |
| 324 | Series 320 for Canadian Pacific Airlines. |
Projected Variants
- Type 175 Series 200
- All-cargo version of Series 100 with 124ft 3in fuselage length. Four 4,120 e.h.p. Bristol Proteus 755 powerplants.
- Type 175 Series 350
- Developed version of the Britannia powered by four Bristol Orion twin-spool turboprops.
- Type 175 Series 400
- Fuselage extended by 10 ft than previous models, and a thinner wing to permit higher operating weights. Four 6,000 b.h.p. Orion Series II turboprops.
- Type 175 Series 553
- Became the Type 195.
- Type 175 Series 600
- Became the Type 187.
- Type 175 Maritime
- Maritime reconnaissance development of the basic Type 175. Four 3,150 s.h.p. Napier Nomad N.Nm. 6 powerplants.
- Type 175MR
- Maritime reconnaissance development with a significantly redesigned fuselage. Four Wright R-3350-32W powerplants.
- Rear-Loading Freighter
- Based on the Series 250 with the rear fuselage was completely redesigned and incorporated a hydraulically operated rear freight-loading door. Four Bristol Proteus 770 powerplants.
- BEWARE
- Britannia Early Warning Airbore Radar Equipment. Type 175 fitted with a 24ft dorsal early warning radar, probably to NASR.6166 and later to ASR.367.
- Type 187
- Joint design study with Convair of San Diego for a 'double-decker' Britannia with thinner and more slender wings. Four Bristol Orion twin-spool turboprops.
- Type 189
- As Type 175MR but fitted with four 3,150 s.h.p. Napier Nomad N.Nm. 6 powerplants.
- Type 195
- High-wing, rear-loading heavy-cargo carrier, using the Britannia wing. Developed into the Short S.C.5 Belfast.
Production Details
| C/n | Initial Registration |
Type | Notes |
| 2 prototype aircraft and one test airframe built by the Bristol Aeroplane Company, Filton, Bristol, to Contract 6/Acft/2460. First flew 16 August 1952. | |||
| 12873 | G-ALBO | 101 | To MoS. Initially registered to MoS as VX442, ntu; registered to MoS as WB470, ntu. |
| 12874 | G-ALRX | 101 | To MoS. Initially registered to MoS as VX447, ntu; registered to MoS as WB473, ntu. |
| 12875 | Not completed, used as functional mockup. Initially registered to MoS as VX454, ntu. | ||
| 15 aircraft built by the Bristol Aeroplane Company, Filton, Bristol. Delivered between December 1955 and May 1957. | |||
| 12902 | G-ANBA | 102 | To BOAC. |
| 12903 | G-ANBB | 102 | To BOAC. |
| 12904 | G-ANBC | 102 | To BOAC. |
| 12905 | G-ANBD | 102 | To BOAC. |
| 12906 | G-ANBE | 102 | To BOAC. |
| 12907 | G-ANBF | 102 | To BOAC. |
| 12908 | G-ANBG | 102 | To BOAC. Changed to G-APLL in March 1958. |
| 12909 | G-ANBH | 102 | To BOAC. |
| 12910 | G-ANBI | 102 | To BOAC. |
| 12911 | G-ANBJ | 102 | To BOAC. |
| 12912 | G-ANBK | 102 | To BOAC. |
| 12913 | G-ANBL | 102 | To BOAC. |
| 12914 | G-ANBM | 102 | To BOAC. To PK-ICA. |
| 12915 | G-ANBN | 102 | To BOAC. To PK-ICB. |
| 12916 | G-ANBO | 102 | To BOAC. |
| 1 prototype aircraft built by the Bristol Aeroplane Company, Filton, Bristol. First flew 31 July 1957. | |||
| 12917 | G-ANCA | 300 | Series 300 prototype. To MoS. |
| 7 aircraft built by Short Brothers and Harland, Belfast. Delivered between November 1957 and August 1960. | |||
| 12918 | XA-MEC | 300 | To Aeronaves de Mexico, Initially named 'Ciudad de Mexico', later 'Tenochtitlan' and later'Acapulco'. Initially G-ANCB before delivery (originally ordered as by BOAC but cld prior to completion). |
| 12919 | XA-MED | 300 | To Aeronaves de Mexico, Initially named 'Mexico City' and later 'Tzintzuntzan'. Initially G-ANCC before delivery (originally ordered as by BOAC but cld prior to completion). To G-ANCC. |
| 12920 | 4X-AGE | 305 | To El Al. Initially G-ANCD before delivery (originally ordered as by BOAC but cld prior to completion, then allocated N6595C for Northeast Airlines but ntu).To G-ANCD; 5Y-AYR. |
| 12921 | G-ANCE | 305 | Leased to Air Charter Ltd. via Bristol Aircraft Ltd. (originally ordered as by BOAC but cld prior to completion, then allocated N6596C for Northeast Airlines but cld). To EI-BAA. |
| 12922 | LV-PPJ | 305 | To Transcontinental S.A., later re-registered LY-GJB. Initially G-ANCF before delivery (originally ordered as by BOAC but cld prior to completion, then allocated N6597C for Northeast Airlines but cld). To G-ANCF; 5Y-AZP; G-ANCF. |
| 12923 | LV-PPL | 305 | To Transcontinental S.A., later re-registered LY-GJC. Initially G-ANCG before delivery (originally ordered as by BOAC but cld prior to completion, then allocated N6598C for Northeast Airlines but cld). To G-ANCG. |
| 12924 | 9G-AAG | 305 | To Ghana Airways. Initially G-ANCG before delivery (originally ordered as by BOAC but cld prior to completion, then allocated N6598C for Northeast Airlines but cld). To G-ANCG; 9G-AAG. |
| 13 aircraft built by the Bristol Aeroplane Company, Filton, Bristol. Delivered between July 1957 and March 1958. | |||
| 12925 | G-AOVH | 310 | To BOAC. |
| 12926 | G-AOVI | 310 | To BOAC. |
| 13207 | G-AMYK | 200 | Not built as such. |
| G-AOFA | 300LR | Not built as such. | |
| G-AOVA | 310 | Series 310 prototype. Leased to BOAC July 1957. To 9G-AAH; G-AOVA. | |
| 13208 | G-AMYL | 200 | Not built as such. |
| G-AOFB | 300LR | Not completed. Most likely became a test airframe. | |
| 13230 | G-AOVB | 310 | To BOAC. To LV-PNJ in October 1969. Re-registered as LV-JNL. |
| 13231 | G-AOFC | 300LR | Not built as such. |
| G-AOVC | 310 | To BOAC. | |
| 13232 | 4X-AGA | 310 | To El Al. To G-ASFV; 4X-AGA; HB-ITB. |
| 13233 | 4X-AGB | 310 | To El Al. To G-ARWZ; 4X-AGB; EC-BFL (ferry regn EC-WFL). |
| 13234 | G-ANGK | 250 | Registered to Bristol Aeroplane Co against possible BOAC order. Not built as such. |
| 4X-AGC | 310 | To El Al. To G-ARXA; 4X-AGC; G-ARXA. | |
| 13235 | G-AOFD | 300LR | Registered to Bristol Aeroplane Co against possible BOAC order. Not built as such. |
| G-AOVD | 310 | To BOAC. | |
| 13236 | G-AOFE | 300LR | Registered to Bristol Aeroplane Co against possible BOAC order. Not built as such. |
| G-AOVE | 310 | To BOAC. To EC-BFK (ferry regn EC-WFK). | |
| 13237 | G-AOFF | 300LR | Registered to Bristol Aeroplane Co against possible BOAC order. Not built as such. |
| G-AOVF | 310 | To BOAC. To 9Q-CAZ. | |
| 13238 | G-AOFG | 300LR | Registered to Bristol Aeroplane Co against possible BOAC order. Not built as such. |
| G-AOVG | 310 | To BOAC. | |
| 4 aircraft built by Short Brothers and Harland, Belfast. Delivered between April and June 1958. | |||
| 13393 | CF-CZA | 310 | To Canadian Pacific. To G-ATGD; 5X-UVT; 5X-ALP. |
| 13394 | CF-CZB | 310 | To Canadian Pacific. |
| 13395 | CF-CZC | 310 | To Canadian Pacific.To G-ATLE. |
| 13396 | CF-CZD | 310 | To Canadian Pacific.To G-ATNZ. |
| 4 aircraft built by Short Brothers and Harland, Belfast. Delivered between June 1959 and January 1960. | |||
| 13397 | XL635 | 253 | To RAF (See Military Table). To OO-YCA. |
| 13398 | XL636 | 253 | To RAF (See Military Table). To OO-YCE. |
| 13399 | XL637 | 253 | To RAF (See Military Table). To OO-YCH. |
| 13400 | XL638 | 253 | To RAF (See Military Table). |
| 16 aircraft built by the Bristol Aeroplane Company, Filton, Bristol. Delivered between April 1958 and March 1959. | |||
| 13418 | G-AOFJ | 300LR | Not built as such. |
| G-AOVJ | 310 | To BOAC. | |
| 13419 | G-AOVK | 310 | To BOAC. |
| 13420 | G-AOVL | 310 | To BOAC. |
| 13421 | G-AOVM | 310 | To BOAC. To EC-BSY. To MoD as XX367 (See Military Table). To 9Q-CHY. |
| 13422 | G-AOVN | 310 | To BOAC. |
| 13423 | G-AOVO | 310 | To BOAC. |
| 13424 | G-AOVP | 310 | To BOAC. |
| 13425 | G-APNA | 310 | To Hunting Clan Air Transport. |
| 13426 | G-APNB | 310 | To Hunting Clan Air Transport. |
| 13427 | G-AOVT | 310 | To BOAC. |
| 13428 | CF-CZX | 310 | To Canadian Pacific. To G-ATMA; 5Y-ANS; G-ATMA. |
| 13429 | G-AOVR | 310 | To BOAC. To EC-BFJ (ferry regn EC-WFJ). |
| 13430 | G-AOVS | 310 | To BOAC. |
| 13431 | 4X-AGD | 310 | To El Al. To G-ASFU; 4X-AGD; HB-ITC; 5X-UVH; 5Y-ALT. |
| 13432 | CU-T668 | 310 | To Cubana (ferry regn CU-P668). To G-APYY; CU-T668; OK-MBA; CU-T668. |
| 13433 | CU-T669 | 310 | To Cubana (ferry regn CU-P669). To CU-T114. |
| 3 aircraft built by Short Brothers and Harland, Belfast. Delivered between May and July 1960. | |||
| 13434 | XM489 | 253 | To RAF (See Military Table). To OO-YCC. |
| 13435 | XM490 | 253 | To RAF (See Military Table). To G-BDLZ. |
| 13436 | XM491 | 253 | To RAF (See Military Table). To EI-BBH; 9QCMO. |
| 1 aircraft built by the Bristol Aeroplane Company, Filton, Bristol. Delivered in May 1959. | |||
| 13437 | CU-T670 | 310 | To Cubana (ferry regn CU-P670). |
| 17 aircraft built by Short Brothers and Harland, Belfast. Delivered between March 1959 and December 1960. | |||
| 13448 | XL639 | 253 | To RAF (See Military Table). To EI-BDC, G-BRAC. |
| 13449 | XL640 | 253 | To RAF (See Military Table). To EI-BCI |
| 13450 | G-APPE | 252 | To MoS. To A&AEE as XN392 (See Military Table). |
| 13451 | G-APPF | 252 | To MoS. To A&AEE as XN398 (See Military Table). To 9Q-CPX. |
| 13452 | G-APPG | 252 | To MoS. To A&AEE as XN404 (See Military Table). |
| 13453 | CF-CZW | 310 | To Canadian Pacific. To G-ASTF;CF-CZW; G-ASTF. |
| 13454 | XL657 | 253 | To RAF (See Military Table). To 9U-BAD. |
| 13455 | XL658 | 253 | To RAF (See Military Table). To EI-BBY. |
| 13456 | XL659 | 253 | To RAF (See Military Table). To OO-YCB. |
| 13457 | XL610 | 253 | To RAF (See Military Table). To G-BEMZ; A6-HMS; G-BEMZ; 9Q-CGP. |
| 13508 | XM496 | 253 | To RAF (See Military Table). To G-BDUP; CU-T120; 9Q-CJH; EI-WXA. |
| 13509 | XM497 | 253 | To RAF (See Military Table). To OO-YCF. |
| 13510 | XM498 | 253 | To RAF (See Military Table). To OO-YCG; EI-LWG; 9Q-CDT. |
| 13511 | XM517 | 253 | To RAF (See Military Table). To 9Q-CAJ, G-BEPX. |
| 13512 | XM518 | 253 | To RAF (See Military Table). To OO-YCD. |
| 13513 | XM519 | 253 | To RAF (See Military Table). To G-BDUR; CU-T121. |
| 13514 | XM520 | 253 | To RAF (See Military Table). To 9G-ACE; 9Q-CUM. |
| 3 aircraft built by the Bristol Aeroplane Company, Filton, Bristol. Delivered betwee August and November 1959. | |||
| 13515 | CU-T671 | 310 | To Cubana (ferry regn CU-)671). To MBB. |
| 13516 | CF-CPD | 320 | To Canadian Pacific. To G-ARKA; HB-ITF ntu. |
| 13517 | CF-CPE | 320 | To Canadian Pacific To G-ARKB; HB-ITG ntu |
| Total Production 85 | |||
Type 175 Britannia In Military Service
| Serial Range | C/n | Type | Batch Qty |
Conv. | Canc'd | Notes |
| 20 aircraft ordered from the Bristol Aeroplane Company, Filton, Bristol, Somerset, to Contract 6/Acft/12829 and built by Short Brothers and Harland, Belfast. Delivered between June 1959 and April 1960. | ||||||
| XL635 - XL640 | 13397-13400, 13448, 13449 | C.1 | 6 | XL635 first flew on 29 December 1958. | ||
| XL657 - XL660 | 13454-13457 | 4 | ||||
| 3 aircraft ordered from the Bristol Aeroplane Company, Filton, Bristol, Somerset, to Contract 6/Acft/14293 and built by Short Brothers and Harland, Belfast. Delivered between May and July 1960. | ||||||
| XM489 - XM491 | 13434-13436 | 3 | ||||
| 7 aircraft ordered from the Bristol Aeroplane Company, Filton, Bristol, Somerset, to Contract 6/Acft/14293 and built by Short Brothers and Harland, Belfast. Delivered between October 1959 and December 1960. | ||||||
| XM496 - XM498 | 13508-13510 | 3 | ||||
| XM517 - XM520 | 13511-13514 | 4 | ||||
| 3 aircraft ordered from the Bristol Aeroplane Company, Filton, Bristol, Somerset, to Contract 6/Acft/11804 and built by Short Brothers and Harland, Belfast. Delivered between March and October 1959. | ||||||
| XN382 | 13450 | C.2 | (1) | Ex-G-APPE | ||
| XN398 | 13451 | (1) | Ex-G-APPF | |||
| XN404 | 13452 | (1) | Ex-G-APPG | |||
| 1 aircraft purchaced to Contract K49A/125. Delivered in May 1972. | ||||||
| XX367 | 13421 | Srs. 312 | (1) | Ex-EC-BSY, G-AOVM | ||
| Total Production | 20 | (4) | ||||
Foreign Derivatives
Canadair Ltd.,Cartierville, Montreal, Canada
CL-28 Variants
CL-28 CP-107 Argus Mk.1
Fifteen crew Maritime Reconnaissance aircraft to RCAF Specification Air 15-11. A derivative of the Type 175, it had the same wings, tail surfaces and landing gear, but changed from British materials, dimensions and standard parts to American ones. Due to the greater stresses from flying at low altitude for long periods of time, the components taken from the Britannia needed substantial reinforcement. The fuselage was completely redesigned, going from the pressure cabin used in the Britannia to an unpressurised one with two 18 ft long bomb bays fore and aft of the wings, each accomodating up to 8,000 lb. of weapons, including torpedoes, bombs and depth charges. Hard points under the wings could carry a variety of other weapons. Fitted with an American APS-20 radar in a chin-mounted radome, along with an 18 ft long Magnetic Anomoly Detector boom extending aft from the rear fuselage. Four 3,700 s.h.p. Wright R-3350 TC18EA1 Turbo-Compound powerplants.
CL-28 CP-107 Argus Mk.2
As Mk.1 fitted with a British ASV-21 radar in a chin-mounted radome
| CL-28 CP-107 Argus Mk.2 Specification | |||||||||
| Span | Length | Height | Wing Area | Empty Wt | Max AUW | Cruise Speed | Maximum Speed | Range | Service Ceiling |
| 142 ft 3 in | 128 ft 3 in | 36 ft 9 in | 2075 sq ft | 81000 lb | 148000 lb | 207 mph/ 180 kn | 290 mph/ 252 kn | 4000 mi | 24200 ft |
| 43.36 m | 39.09 m | 11.2 m | 192.77 m2 | 36741 kg | 67132 kg | 333 km/h | 467 km/h | 6437 km | 7376 m |
Canadair CL-28 Argus Production Details
| Serial Range | C/n | Type | Batch Qty |
Conv. | Canc'd | Notes |
| 33 aircraft ordered from Canadair Ltd.,Cartierville, Montreal, Canada, for the RCAF. Delivered between May 1957 to November 1960. | ||||||
| 20710 - 20722 | 1-13 | CP-107 Argus Mk.1 | 13 | From May 1970 serialled 10710 - 10722 in the Canadian Air Force. | ||
| 20723 - 20742 | 14-33 | CP-107 Argus Mk.2 | 20 | From May 1970 serialled 10723 - 10742 in the Canadian Air Force. | ||
| Total Production | 33 | |||||
CL-44 Variants (See Note 1)
CL-44-6 CC-106 Yukon
Military transport, with the fuselage largely based on the Britannia Series 300, but lengthened by 12 ft 4 in, and capable of carrying 134 passengers, 80 stretchers or over 60,000 lb of cargo. It featuring two large cargo doors fore and aft on the port side, and used modified CL-28 wings, empennage and controls, with redesigned landing gear to accomodate the higher weights. Originally intended to be fitted with Bristol Orions but revised for four 5,500 e.s.h.p. Rolls Royce Tyne 11 powerplants.
CL-44D4
Commercial cargo transport. As CL-44-6 but featuring swing tail rear cargo entry with an Integrated Air Cargo System fitted to enable fast loading and unloading of palletised or containerised cargo. The CL-44-6's forward port side cargo door was retained, a passenger door replacing the aft. A new cockpit windscreen was fitted, based on that of the Convair 880/990. Four 5,730 e.s.h.p. Rolls Royce Tyne 12 powerplants.
CL-44J
Passenger carrying variant of the CL-44D4, without the swing tail feature. The fuselage was stretched by 10 ft 1 in forward of the wing and another section of 5 ft 1 in aft, bringing the capacity to 189 passengers.
| CL-44D4 Specification | |||||||||
| Span | Length | Height | Wing Area | Empty Wt | Max AUW | Cruise Speed | Maximum Speed | Range | Service Ceiling |
| 142 ft 3 in | 136 ft 10 in | 37 ft 5 in | 2075 sq ft | 88876 lb | 210000 lb | 386 mph/ 335 kn | 320 mph/ 278 kn | 5640 mi | 30000 ft |
| 43.36 m | 41.71 m | 11.4 m | 192.77 m2 | 40313 kg | 95254 kg | 621 km/h | 515 km/h | 9077 km | 9144 m |
CL-44 Projected Variants (See Note 1)
- CL-44
- Military Transport. Four Wright 981 powerplants.
- CL-44-1
- Military Transport. Four Tyne 2 powerplants.
- CL-44-1A
- Military Transport. Four Orion powerplants.
- CL-44-1B
- Military Transport. Four Orion powerplants.
- CL-44-2
- Military Transport. Four Tyne 2 powerplants.
- CL-44-3
- Military Transport. Four Orion powerplants.
- CL-44-4
- Military Transport. Four Orion powerplants.
- CL-44-5
- Military Transport. Four Tyne 10 powerplants.
- CL-44-7
- Arctic Reconnaissance. Four Tyne 12 powerplants.
- CL-44-8
- Military Cargo/Passenger Transport, Swingtail. Four Tyne 12 powerplants.
- CL-44-9
- Military Transport Army Vehicle Carrier, Swingtail. Four Tyne 12 powerplants.
- CL-44A
- Military Transport. Four Proteus 755 powerplants.
- CL-44B
- Military Transport. Four Orion powerplants.
- CL-44C
- Commercial Transport, 200,000 lbs (later 208,000 lbs). Four Orion powerplants.
- CL-44D
- Commercial Transport. Four Tyne 12 powerplants.
- CL-44D-1
- Commercial Transport. Four Tyne 12 powerplants.
- CL-44D-2
- Commercial Transport, Cargo only, tail-loading. Four Tyne 12 powerplants.
- CL-44D-3
- Commercial Transport, Cargo/Passenger. Four Tyne 12 powerplants.
- CL-44D-4
- Commercial Transport. Four Tyne 12 powerplants.
- CL-44D4-3
- Cargo/Passenger Transport for Flying Tiger Line. Four Tyne 12 powerplants.
- CL-44D4-4
- Cargo Tansport for Pan American World Airways. Four Tyne 12 powerplants.
- CL-44D4-5
- Military Cargo/Passenger for MATS/USAF. Four Tyne 12 powerplants.
- CL-44D4-7
- Long-range Cargo Transport 3 for Pan American World Airways. Four Tyne 12 powerplants.
- CL-44D4-8
- Commercial Cargo Transport, tail-loading. Four Tyne 12 powerplants.
- CL-44D5-1
- Medium-range Cargo Transport, 205,000 lbs gross take-off weight. Four Tyne 14 powerplants.
- CL-44D5-2
- Medium-range Cargo Transport 210,000 lbs gross take-off weight. Four Tyne 12 powerplants.
- CL-44D6
- Long-range Cargo Transport, 225,000 lbs gross take-off weight, tail-loading. Four Stage 4 Tyne powerplants.
- CL-44D7
- Long-range Cargo Transport, 225,000 lbs gross take-off weight, tail-loading. Four Tyne 14 powerplants.
- CL-44D8
- Long-range Cargo Transport, 225,000 lbs gross take-off weight, tail-loading. Four Stage 4 Tyne powerplants.
- CL-44D9
- Long-range Cargo Transport, 2250,000 lbs gross take-off weight, tail-loading. Four Stage 4 Tyne powerplants.
- CL-44D10
- Long-range Cargo Transport, mechanised cargo loading for container and pallets. Four Tyne 14 powerplants.
- CL-44D11
- Domestic version of CL-44D10, 205000 lbs.
- CL-44D12
- Overseas version of CL-44D10 215000 lbs.
- CL-44E
- Commercial Transport. Four Stage 3 Tyne powerplants.
- CL-44F
- Commercial Transport with CL-44-4 wing. Four Tyne 12 powerplants.
- CL-44G
- Military Transport, tail-loading. Four Tyne 11 powerplants.
- CL-44G-1
- Military Transport, tail-loading, for Royal Air Force. Four Tyne 12 powerplants.
- CL-44H
- Long-range Cargo Transport, tail-loading. Four Stage 4 Tyne powerplants.
- CL-44H1
- Long-range Cargo Transport, tail-loading, low cargo-density fuselage. Four Stage 4 Tyne powerplants.
- CL-44H2
- Long-range Cargo Transport, tail-loading, medium cargo-density fuselage. Four Stage 4 Tyne powerplants.
- CL-44H3
- Long-range Cargo Transport, tail-loading, high cargo-density fuselage. Four Stage 4 Tyne powerplants.
- CL-44H4
- Long-range Cargo Transport, tail-cone loading, low cargo-density fuselage. Four Stage 4 Tyne powerplants.
- CL-44H5
- Long-range Cargo Transport, tail-loading. Four Stage 4 Tyne powerplants.
- CL-44H6
- Long-range Cargo Transport, tail-loading. Four Stage 4 Tyne powerplants.
- CL-44K
- Long-range Cargo/Passenger transport, 210.000 lbs gross take-off weight. Four Tyne 12 powerplants.
- CL-44L
- Long-range Cargo transport, extended fuselage. Four Tyne 12 powerplants.
- CL-44W
- Early Warning and Control variant. Four Allison 550 B-1 powerplants.
Canadair CL-44 Production Details
| C/n | Initial Registration |
Type | Notes |
| 39 aircraft built by Canadair Ltd.,Cartierville, Montreal, Canada, between November 1959 and March 1965. | |||
| 1 | 15921 | CL-44-6 | To RCAF (See Military Table). To Beaver Enterprises as CF-DSY. To C-FDSY; YS-04C; HK-1972. |
| 2 | 15922 | CL-44-6 | To RCAF (See Military Table). To Société Générale d'Alimentation as 9Q-CWN, named "Hoto Meyo". |
| 3 | 15923 | CL-44-6 | To RCAF (See Military Table). To Canhellas as CF-CHC. To HC-AYS. |
| 4 | 15924 | CL-44-6 | To RCAF (See Military Table). To Aerotransportes Entre Rios as LV-LBS. |
| 5 | 15925 | CL-44-6 | To RCAF (See Military Table). To Aerotransportes Entre Rios as LV-JSY (ferry regn LV-PQL). |
| 6 | 15926 | CL-44-6 | To RCAF (See Military Table). To Aerotransportes Entre Rios as LV-JZR. To OB-R-1005; 9Q-CKQ. |
| 7 | 15927 | CL-44-6 | To RCAF (See Military Table). To Aerotransportes Entre Rios as LV-JYR. |
| 8 | 15928 | CL-44-6 | To RCAF (See Military Table). To Transportes Aéreo Rioplatense as LV-JZB (ferry regn LV-PRX). To CX-BKD. |
| 9 | TF-LLH | CL-44D4-1 | To Loftleiðir, named 'Gudridur Thorbjarnardottir'. Initially CF-MKP-X before delivery. Converted to CL-44J by Canadair in 1965. To EI-BGO. |
| 10 | 15929 | CL-44-6 | To RCAF (See Military Table). To International Air Leases as C-GADY, via Beaver Enterprises. To 9Q-CWS. |
| 11 | 15930 | CL-44-6 | To RCAF (See Military Table). To Societe Generale d'Alimentation via Beaver Enterprises as 9Q-CWK, named "Gegitelo". |
| 12 | 15511 | CL-44-6 | To RCAF (See Military Table). To Batchair as C-GACH, via International Air Leases. To OB-R-1104. |
| 13 | 15512 | CL-44-6 | To RCAF (See Military Table). To Beaver Enterprises as CF-JSN. To HC-AZH. |
| 14 | N124SW | CL-44D4-1 | To Seaboard and Western Airlines. Initially CF-MYO-X before delivery. To G-AWUD ntu; TF-CLA;TR-LWF; HC-BHS. |
| 15 | N446T | CL-44D4-2 | To Flying Tiger Line. Scheduled to be converted to CL-44-O by Conroy, but crashed before delivery. |
| 16 | N447T | CL-44D4-2 | To Flying Tiger Line. Converted to the sole CL-44-O by Conroy. To EI-BND; 4K-GUP; P4-GUP ntu; 9G-LCA; N440CC ntu; RP-C8023 |
| 17 | N448T | CL-44D4-2 | To Flying Tiger Line. To G-AWWB; VR-HHC; G-AWWB; N908L; N200TK ntu. |
| 18 | N449T | CL-44D4-2 | To Flying Tiger Line. To G-AXAA; N122AE. |
| 19 | N450T | CL-44D4-2 | To Flying Tiger Line. Initially CF-NBP-X before delivery. To G-AZIN; PK-BAW |
| 20 | N451T | CL-44D4-2 | To Flying Tiger Line. Initially CF-NND-X before delivery. To TF-LLJ; OO-ELJ; TR-LVO. |
| 21 | N452T | CL-44D4-2 | To Flying Tiger Line. Initially CF-NNE-X before delivery. To G-ATZH |
| 22 | N44853 | CL-44D4-2 | To Flying Tiger Line. |
| 23 | N125SW | CL-44D4-1 | To Seaboard and Western Airlines. Initially CF-NNM-X before delivery. To G-AWDK; PK-BAZ. |
| 24 | N454T | CL-44D4-2 | To Flying Tiger Line. To G-AXUL; N104BB; 9U-BHI; 3C-ZPO |
| 25 | N455T | CL-44D4-2 | To Flying Tiger Line. To G-ATZI ntu; HB-IEN; 5A-DHG; 5A-DHJ; N3951C; 9Q-CQU; N103BB; EI-WLL; TN-AFP; 9Q-CTS. |
| 26 | N126SW | CL-44D4-1 | To Seaboard and Western Airlines. To G-AWSC; N126SW; G-AWSC. |
| 27 | N127SW | CL-44D4-1 | To Seaboard and Western Airlines. To G-AWGS; N127SW; G-AWGS; N907L |
| 28 | N602SA | CL-44D4-6 | To Slick Airways. Initially CF-NYC-X before delivery. To VP-LAT; N62163; G-BCWJ |
| 29 | N603SA | CL-44D4-6 | To Slick Airways. To N100BB. |
| 30 | N128SW | CL-44D4-1 | To Seaboard and Western Airlines. To G-AWGT; N123SW; G-AWGT; 5B-DAN |
| 31 | N228SW | CL-44D4-1 | To Seaboard and Western Airlines. Initially CF-OFH-X before delivery. |
| 32 | N229SW | CL-44D4-1 | To Seaboard and Western Airlines. To G-AWOV; N429SW; G-AWOV; HB-IEO; 5A-DGE. |
| 33 | N604SA | CL-44D4-6 | To Slick Airways. To LV-JZM. |
| 34 | N605SA | CL-44D4-6 | To Slick Airways. To LV-JZN; CX-BML ntu; LV-JTN |
| 35 | TF-LLF | CL-44D4-8 | To Loftleiðir, named 'Leifur Eiriksson'. Initially CF-PBG-X before delivery. Converted to CL-44J by Canadair in 1965. To N4993U; 5A-CVB; 5A-DGJ; 9Q-CQS; EI-BRP. |
| 36 | TF-LLG | CL-44D4-8 | To Loftleiðir, named 'Vilhjálmur Stefánsson'. Converted to CL-44J by Canadair in 1965. |
| 37 | N1001T | CL-44D4-2 | To Flying Tiger Line. Initially CF-PZZ-X before delivery. To G-AZKJ; G-BRED; N106BB; EI-AMC; 7Q-YMS; TN-235 ntu; TN-AFC (not confirmed). |
| 38 | N1002T | CL-44D4-2 | To Flying Tiger Line. Initially CF-RLS-X before delivery. To G-AZM; N121AE. |
| 39 | TF-LLI | CL-44D4-8 | Converted to CL-44J before delivery. To Loftleiðir, named 'Bjarni Herjólfsson'. Initially CF-SEE-X before delivery. To TF-LLI; CX-BJV; N4998S HK-3148X. |
| Total Production 39 | |||
Canadair CC-106 Yukon Production
| Serial Range | C/n | Batch Qty |
Conv. | Canc'd | Notes |
| 12 aircraft ordered from Canadair Ltd.,Cartierville, Montreal, Canada, for the RCAF. Delivered between May 1957 to November 1960. | |||||
| 15921 - 15928 | 1-8 | 8 | 15921 - 15923 originally 15501-15503, renumbered on 30 Sep 1960; to CAF 106921 - 106923 on 26 May 1970. 15924 - 15928 allocated 15504-15508, renumbered before delivery; to CAF 106924 - 106928 on 26 May 1970 |
||
| 15929 - 15932 | 10-13 | 4 | 15929 became 15555 on 14 April 1961, back to 15929 on 1 May 1962; to CAF 106929 on 26 May 1970. 15930 - 15932 allocated 15510 - 15512, renumbered before delivery; to CAF 106930 - 106932 on 26 May 1970. |
||
| Total Production | 12 | ||||
Conroy Aircraft Corporation, Goleta, California, USA.
- CL-44-O
- Also known as the Skymonster and CL-44 Guppy. One CL-44D4-2 (c/n 15), which type it officially remained, with the fuselage shell removed above the floorline, and rebuilt with enlarged fuselage to create a cargo aircraft for oversize loads, the nose section of which was built using foam covered with fiberglass, while the larger fuselage was constructed using conventional aluminum structure. Modified under STC number SA2183WE, issued to “RJWJ Corporation, a California Corporation”.
Production Summary
Bristol Production - All Aircraft By Series
| Type | Built New | Conv | Canc'd | Total |
| Type 175 Britannia Series 101 | 2 | 2 | ||
| Type 175 Britannia Series 102 | 15 | 15 | ||
| Type 175 Britannia Series 200 | 2 | 2 | ||
| Type 175 Britannia Series 250 | 1 | 1 | ||
| Type 175 Britannia C.2 (Series 252) | 3 | 3 | ||
| Type 175 Britannia C.1 (Series 253) | 20 | 20 | ||
| Type 175 Britannia Series 300 | 3 | 3 | ||
| Type 175 Britannia Series 300LR | 8 | 8 | ||
| Type 175 Britannia Series 305 | 5 | 5 | ||
| Type 175 Britannia Series 310 | 35 | 35 | ||
| Type 175 Britannia Series 320 | 2 | 2 | ||
| 85 | (0) | 11 |
Canadair Production - All Aircraft By Type
| Type | Built New | Conv | Canc'd | Total |
| CL-28 Argus Mk.1 | 13 | 13 | ||
| CL-28 Argus Mk.2 | 20 | 20 | ||
| CL-44-6 Yukon | 12 | 12 | ||
| CL-44D4-1 | 8 | 8 | ||
| CL-44D4-2 | 12 | 12 | ||
| CL-44D4-6 | 4 | 4 | ||
| CL-44D4-8 | 3 | 3 | ||
| CL-44J | (4) | 4 | ||
| CL-44-O | (1) | 1 | 2 | |
| 72 | (5) | 1 |
Production References
- Bristol Aircraft Since 1910, C.H. Barnes (Putnam, 1964, 1970 and 1988)
- Bristol Britannia, Charles Woodley (The Crowood Press Ltd, 2002)
- The Bristol 170, Britannia, Canadair CL-28 and CL-44, Peter Davis and Stephen Piercey (Air-Britain (Historians), 1977)
- Canadian Aircraft Since 1909, K.M. Molson and H.A. Taylor (Putnam, 1982)
- Turboprop Airliners of the World 1949-2012, Terry Smith (Air Britain (Historians), 2012)
- Aviation News Mini-Monograph - Bristol Britannia in Royal Air Force Service, Paul A. Jackson (Alan W Hall Publications, 1981)
- Royal Air Force Aircraft XA100-XZ999, RAF Aircraft Register Series, J.J. Halley (Air-Britain Publications, 2001)
- British Military Aircraft Serials and Markings, British Aviation Research Group (BARG/Nostalgair, 1983)
- Air Britain Archive 2013/1, (Air-Britain Publications)
- Air Enthusiast 20
- Canadian Military Aircraft Serial Numbers at CASPIR (Canadian Aircraft Serials Personnel Information Resource) at the Canadian Warplane Heritage Museum
- Western-built aircraft in Soviet & Eastern Block service
- The Canadair CL44
- https://www.airvectors.net
- The CL-44 Story, Malcolm Porter (Air Britain Historians Ltd, 2004)
- Canadair - The First 50 Years, Ron Pickler and Larry Milberry (CANAV Books, 1995)
Page Revision History
Revised at Version 2.1.0- CL-28 and CL-44 Type Details, Projects and Specifications updated/added.
- Improved Type Description and Added Specification details.
- Britannia C.1 Contracts corrected.